1 February 2003, 0900:18 EST: Space Shuttle Columbia, nearing the end of Mission STS-107, traveling Mach 19.5 (13,434 miles per hour, 21,620 kilometers per hour) at 209,800 feet (63,950 meters) over Texas, suffered catastrophic structural failure and disintegrated. All seven members of her crew were killed.
81.7 seconds after liftoff on 16 January, Columbia was at approximately 66,000 feet (20,100 meters) altitude and 12.5 miles (20.1 kilometers) down range, accelerating through Mach 2.46 (1,623 miles per hour, 2,612 kilometers per hour). Several pieces of insulating foam broke off of the external fuel tank (what NASA referred to as “foam shedding”) and struck the leading edge and underside of Columbia‘s left wing. It is believed that at least one of these pieces of foam punctured a hole in the wing’s surface, estimated to be 6 inches × 10 inches (15 × 25 centimeters).
During reentry, the internal structure of the wing was no longer protected by the heat resistant material of the leading edge. The extreme heat caused structural failure.
Columbia (OV-102) was America’s first space shuttle. It flew into space for the first time 11 April 1981. STS-107 was its 28th flight. During those missions, Columbia orbited the Earth 4,808 times and spent 300 days, 17 hours, 40 minutes, 22 seconds in space flight. 160 astronauts served aboard her. She traveled 125,204,911 miles (201,497,722 kilometers).
1 February 1975: Major Roger J. Smith, United States Air Force, a test pilot assigned to the F-15 Joint Test Force at Edwards AFB, California, flew the McDonnell Douglas F-15A-6-MC 72-0119, Streak Eagle, to its eighth Fédération Aéronautique Internationale (FAI) and U.S. National Aeronautic Association time-to-altitude record.
From brake release at Grand Forks Air Force Base, North Dakota, at 913 feet (278 meters) above Sea Level, the F-15 reached 30,000 meters (98,425 feet) in 3 minutes, 27.799 seconds.
This was the eighth time-to-altitude record set by Streak Eagle in 17 days.
FAI Record File Num #8520 [Direct Link]
Status: ratified – retired by changes of the sporting code
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Time to climb to a height of 30 000 m
Performance: 3 min 27.799s
Course/Location: Grand Forks, ND (USA)
Claimant Roger J. Smith (USA)
Aeroplane: McDonnell Douglas F-15
Engines: 2 Pratt & Whitney F-100
The flight profiles for the record attempts were developed by McDonnell Douglas Chief Developmental Test Pilot, Charles P. “Pete” Garrison (Lieutenant Colonel, U.S. Air Force, Retired).
Streak Eagle carried only enough fuel for each specific flight. It was secured to the hold-back device on the runway and the engines were run up to full afterburner. It was released from the hold-back and was airborne in just three seconds.
When the F-15 reached 428 knots (793.4 kilometers per hour), the pilot pulled up into an Immelmann turn, holding 2.5 Gs. Streak Eagle would arrive back over the air base in level flight at about 32,000 feet (9,754 meters), but upside down. Rolling right side up, Streak Eagle continued accelerating to Mach 1.5 while climbing through 36,000 feet (10,973 meters). It would then accelerate to Mach 2.2 and the pilot would pull the fighter up at 4.0 Gs until it reached a 60° climb angle. He held 60° until he had to shut down the engines to prevent them from overheating in the thin high-altitude atmosphere.
After reaching a peak altitude and slowing to just 55 knots (63 miles per hour, 102 kilometers per hour), the airplane was pushed over into a 55° dive. Once it was below 55,000 feet (16,764 meters) the engines would be restarted and Streak Eagle returned to land at Grand Forks.
Streak Eagle is a very early production F-15A-6-MC Eagle, a single-seat, twin-engine air superiority fighter. It is 63 feet, 9 inches (19.431 meters) long with a wingspan of 42 feet, 9½ inches (13.043 meters) and overall height of 18 feet, 5½ inches (5.626 meters). The F-15A has an empty weight of 27,000 pounds (12,247 kilograms) and its maximum takeoff weight (MTOW) is 66,000 pounds (29,937 kilograms).
The F-15A is powered by two Pratt & Whitney JTF22A-25A (F100-PW-100) afterburning turbofan engines capable of producing 14,670 pounds of thrust (65.255 kilonewtons), and 23,830 pounds (105.996 kilonewtons), each, with afterburner. The F100 is a two-spool, axial-flow turbine engine with a 3-stage fan section; 10-stage compressor; single chamber combustion section; and 4-stage turbine (2 low- and 2 high-pressure stages). The F100-PW-100 is 191 inches (4.851 meters) long, 46.5 inches (1.181 meters) in diameter, and weighs 3,035 pounds (1,376.7 kilograms).
The cruise speed of the F-15A Eagle is 570 miles per hour (917 kilometers per hour). It has a maximum speed of 915 miles per hour (1,473 kilometers per hour) at Sea Level, and 1,650 miles per hour (2,655 kilometers per hour) at 36,000 feet (10,973 meters). The service ceiling is 65,000 feet (19,812 meters). It can climb in excess of 50,000 feet per minute (254 meters per second), and with a thrust-to-weight ratio of 1.15:1, could climb straight up. The Eagle’s combat radius is 1,222 miles (1,967 kilometers).
The F-15A is armed with one General Electric M61A1 Vulcan 20mm rotary cannon with 940 rounds of ammunition, four AIM-7 Sparrow radar-guided missiles and four AIM-9 Sidewinder heat-seeking missiles.
384 F-15A Eagles were built before production shifted to the improved F-15C version. As F-15Cs became operational, the F-15As were transferred to Air National Guard units assigned to defend continental U.S. airspace. The last F-15A was retired from service in 2009.
Streak Eagle was specially modified for the record attempts. Various equipment that would not be needed for these flights was eliminated: The flap and speed brake actuators, the M61A1 Vulcan 20 mm cannon and its ammunition handling equipment, the radar and fire control systems, unneeded cockpit displays and radios, and one generator.
Other equipment was added: A long pitot boom was mounted at the nose with alpha and beta vanes, equipment for the pilot’s David Clark Company A/P-225-6 full pressure suit, extremely sensitive accelerometers and other instrumentation, extra batteries, an in-cockpit video camera aimed over the pilot’s shoulder, and perhaps most important, a special hold-down device was installed in place of the fighter’s standard arresting hook.
These changes resulted in an airplane that was approximately 1,800 pounds (817 kilograms) lighter than the standard production F-15A. This gave it a thrust-to-weight ratio of 1.4:1.
Because Streak Eagle was a very early production airplane its internal structure was weaker than the final production F-15A standard. It was considered too expensive to modify it to the new standard, so it was transferred to the National Museum of the United States Air Force at Wright-Patterson Air Force Base, Ohio, in December 1980.
1 February 1971: The 4,000th McDonnell Douglas F-4 Phantom II, F-4E-44-MC serial number 69-7294, was delivered to the United States Air Force.
In 1989, 69-7294 was converted to the F-4G Wild Weasel V standard. The Wild Weasel was an aircraft configured to attack surface-to-air missile sites and targeting radars, using a variety of high-speed radar-homing missiles. The F-4G had its M-61 Vulcan rotary cannon removed and replaced with a radar homing and warning radar, as well as improvements to the rear cockpit for management of electronic warfare systems. 134 F-4E Phantom II fighters were converted to F-4G Wild Weasels.
69-7294 served with the U.S. Air Force 90th Tactical Fighter Squadron, 3rd Tactical Fighter Wing at Clark Air Base in the Philippines and in Southwest Asia during the Gulf War as part of the “Philippine Expeditionary Force” and later in Operation Southern Watch with the 190th Fighter Squadron, Idaho Air National Guard. After twenty-five years, 7294 was retired to The Boneyard at Davis-Monthan Air Force Base, Tucson, Arizona in 1996.
The Wild Weasel was next converted to a QF-4G drone. Removed from long term storage and returned to airworthy condition by the Aircraft Maintenance and Regeneration Center, 7294 was flown to Mojave Airport, California, where the drone conversion was completed by Tracor, Inc. Launched from Tyndall Air Force Base, Florida, 69-7294 was “expended” as a remote-controlled aerial target, 4 November 1998.
1 February 1943: During World War II, the 414th Bombardment Squadron (Heavy), 97th Bombardment Group (Heavy), 12th Air Force, U.S. Army Air Forces, was on a mission to attack the docks at the port of Tunis in order to cut the supply chain to the German and Italian armies operating in Tunisia.
A single-engine Messerschmitt Bf 109G fighter defending the city collided with All American III, a Boeing B-17F-5-BO Flying Fortress, serial number 41-24406, which was under the command of Lieutenant Kendrick R. Bragg, Jr., U.S. Army Air Corps. The fighter cut diagonally through the bomber’s fuselage, carried away the left horizontal stabilizer and elevator, and damaged the flight control cables.
The rugged design and construction that made the Flying Fortress a legend allowed the airplane to fly another 90 minutes to its home base at Biskra Airfield, Algeria. Lieutenant Bragg made a careful landing, holding the tail off the runway as long as possible. None of the ten men aboard were injured.
All American III was repaired and was returned to service. It was reassigned to the 352nd Bombardment Squadron (Heavy), 301st Bombardment Group (Heavy) at St. Donat, Tunisia, and flew till nearly the end of the war. It was dismantled for salvage at Lucera Airfield, Italy, 6 March 1945.
41-24406 was assigned to the 92nd Bombardment Group at Bangor, Maine, 13 July 1942. It was flown across the Atlantic Ocean to RAF Polebrook, and reassigned to the 414th. The B-17 arrived at Maison Blanche, Algeria, 13 November 1942. It then traveled to Tafaroufi, Algeria, and then to Biskra, arriving there on Christmas Day.
The Boeing B-17F Flying Fortress was a four-engine heavy bomber operated by a flight crew of ten. It was 74 feet, 9 inches (22.784 meters) long with a wingspan of 103 feet, 9.375 inches (31.633 meters) and an overall height of 19 feet, 1 inch (5.187 meters). Its empty weight was 34,000 pounds (15,422 kilograms), 40,437 pounds (18,342 kilograms) loaded, and the maximum takeoff weight was 56,500 pounds (25,628 kilograms).
The B-17F was powered by four air-cooled, supercharged, 1,823.1-cubic-inch-displacement (29.876 liters) Wright Cyclone C9GC (R-1820-97) nine-cylinder radial engines with turbochargers, producing 1,200 horsepower at 2,500 r.p.m. for takeoff and 1,000 horsepower at 2,300 r.p.m. at Sea Level. War Emergency Power was 1,380 horsepower. The Cyclones turned three-bladed constant-speed Hamilton-Standard Hydromatic propellers with a diameter of 11 feet, 7 inches (3.835 meters) though a 0.5625:1 gear reduction. The R-1820-97 engine is 47.80 inches (1.214 meters) long and 55.10 inches (1.399 meters) in diameter. It weighs 1,315 pounds (596 kilograms).
These engines gave the B-17F a cruising speed of 200 miles per hour (322 kilometers per hour). The maximum speed was 299 miles per hour (481 kilometers per hour) at 25,000 feet, though with War Emergency Power, the bomber could reach 325 miles per hour (523 kilometers per hour) at 25,000 feet for short periods.
The service ceiling was 37,500 feet (11,430 meters). With a normal fuel load of 2,520 gallons (9,540 liters) the B-17F had a maximum range of 2,880 miles (4,635 kilometers). Carrying a 6,000 pound (2,722 kilogram) bomb load, the range was 1,300 miles (2,092 kilometers).
The B-17F Flying Fortress was armed with up to 13 Browning AN-M2 .50-caliber machine guns. Power turrets mounting two guns each were located at the dorsal and ventral positions. The maximum bomb load was 20,800 pounds (9,435 kilograms) over very short ranges. Normally, 4,000–6,000 pounds (1,815–2,722 kilograms) of bombs were carried. The internal bomb bay could be loaded with a maximum of eight 1,600 pound (725.75 kilogram) bombs. Two external bomb racks mounted under the wings between the fuselage and the inboard engines could carry one 4,000 pound (1,814.4 kilogram) bomb, each, though this option was rarely used.
The B-17 Flying Fortress first flew in 1935, and was in production from 1937 to 1945. 12,731 B-17s were built by Boeing, Douglas Aircraft Company and Lockheed-Vega. (The manufacturer codes -BO, -DL and -VE follows the Block Number in each airplane’s type designation.) 3,405 of the total were B-17Fs, with 2,000 built by Boeing, 605 by Douglas and 500 by Lockheed-Vega.
Only three B-17F Flying Fortresses remain in existence.